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A series of small scientific satellite with flexible standard bus

Authors :
Saito, Hirobumi
Sawai, Syujiro
Sakai, Shin-ichiro
Fukuda, Seisuke
Kitade, Kenji
Source :
Acta Astronautica. Nov2009, Vol. 65 Issue 9/10, p1345-1359. 15p.
Publication Year :
2009

Abstract

Abstract: Japan Aerospace Exploration Agency has a plan to develop the small satellite standard bus for various scientific missions and disaster monitoring missions. The satellite bus is a class of 250–400kg mass with three-axis control capability of accuracy. The science missions include X-ray astronomy missions, planetary telescope missions, and magnetosphere atmosphere missions. In order to adapt the wide range of mission requirements, the satellite bus has to be provided with flexibility. The concepts of modularization, reusability, and product line are applied to the standard bus system. This paper describes the characteristics of the small satellite standard bus which will be firstly launched in 2011. [Copyright &y& Elsevier]

Details

Language :
English
ISSN :
00945765
Volume :
65
Issue :
9/10
Database :
Academic Search Index
Journal :
Acta Astronautica
Publication Type :
Academic Journal
Accession number :
44101128
Full Text :
https://doi.org/10.1016/j.actaastro.2009.03.065